Narrative:

During engine start the first officer placed the number 1 engine start switch to start and; shortly thereafter; the tow bar broke. Crew checked the a pump off; but the [low pressure] light was out and 3;000 psi was showing on the gauge when it should have been zero. The engine start was aborted and the speedbrake was deployed to bleed off pressure. Aircraft returned to the gate and maintenance was notified. Maintenance described the problem as a hydraulic engine driven pump solenoid failure causing the system to pressurize when not commanded. Maintenance replaced the solenoid and flight continued.

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Original NASA ASRS Text

Title: A B737-700 returned to the gate after a failed solenoid in the A System engine driven hydraulic pump switch allowed the system to be pressurized during engine start which resulted in a broken tow bar.

Narrative: During engine start the First Officer placed the number 1 engine start switch to start and; shortly thereafter; the tow bar broke. Crew checked the A pump off; but the [low pressure] light was out and 3;000 PSI was showing on the gauge when it should have been zero. The engine start was aborted and the speedbrake was deployed to bleed off pressure. Aircraft returned to the gate and Maintenance was notified. Maintenance described the problem as a hydraulic engine driven pump solenoid failure causing the system to pressurize when not commanded. Maintenance replaced the solenoid and flight continued.

Data retrieved from NASA's ASRS site as of April 2012 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.